Inventor · disambiguated record
Alexandre Forestier
Also filed as: FORESTIER ALEXANDRE
22 granted patents·789 citations·filing 1982–2002
97Inventor score
Top patents by PatentIndex Score
22 records- 0192US4940386AMultiple flow turbojet engine with an outer ring of the fan outlet shrunk onto the caseSNECMA·Filed 1988·Granted Jul 10, 1990·90 cites·5 claims
- 0290US6668559B2Fastening a CMC combustion chamber in a turbomachine using the dilution holesSNECMA MOTEURS·Filed 2002·Granted Dec 30, 2003·76 cites·11 claims
- 0384US4999996ASystem for mounting a pre-vaporizing bowl to a combustion chamberMOTEURS D AVIAT S N E M A SOC·Filed 1989·Granted Mar 19, 1991·52 cites·10 claims
- 0484US4451110ATurbine bearingSNECMA·Filed 1982·Granted May 29, 1984·56 cites·3 claims
- 0581US4494909ADamping device for turbojet engine fan bladesSNECMA·Filed 1982·Granted Jan 22, 1985·50 cites·4 claims
- 0679US6732532B2Resilient mount for a CMC combustion chamber of a turbomachine in a metal casingSNECMA MOTEURS·Filed 2002·Granted May 11, 2004·24 cites·13 claims
- 0779US4449607ASoundproofing for a gas pipe, in particular for the fan jet of a turbojet, and equipment for its fabricationSNECMA·Filed 1982·Granted May 22, 1984·34 cites·8 claims
- 0878US6708495B2Fastening a CMC combustion chamber in a turbomachine using brazed tabsSNECMA MOTEURS·Filed 2002·Granted Mar 23, 2004·44 cites·12 claims
- 0978US4858721AAcoustic panel for sound insulating linings of gas ductsSNECMA·Filed 1988·Granted Aug 22, 1989·48 cites·6 claims
- 1078US4820120AStator assembly for the fan of a multi-flow turbo-jet engineSNECMA·Filed 1987·Granted Apr 11, 1989·39 cites·3 claims
- 1177US4527952ADevice for locking a turbine rotor bladeSNECMA·Filed 1982·Granted Jul 9, 1985·44 cites·10 claims
- 1274US6679062B2Architecture for a combustion chamber made of ceramic matrix materialSNECMA MOTEURS·Filed 2002·Granted Jan 20, 2004·38 cites·10 claims
- 1373US6823676B2Mounting for a CMC combustion chamber of a turbomachine by means of flexible connecting sleevesSNECMA MOTEURS·Filed 2002·Granted Nov 30, 2004·35 cites·12 claims
- 1471US6675585B2Connection for a two-part CMC chamberSNECMA MOTEURS·Filed 2002·Granted Jan 13, 2004·36 cites·9 claims
- 1566US6647729B2Combustion chamber provided with a system for fixing the chamber end wallSNECMA MOTEURS·Filed 2002·Granted Nov 18, 2003·27 cites·13 claims
- 1664US5159807AControl system for oxidizer intake diaphragmsSNECMA·Filed 1991·Granted Nov 3, 1992·23 cites·18 claims
- 1763US4453891AVibration damping device, especially for a blade of a turbojet engineSNECMA·Filed 1982·Granted Jun 12, 1984·19 cites·7 claims
- 1861US5172545AApparatus for attaching a pre-atomization bowl to a gas turbine engine combustion chamberSNECMA·Filed 1991·Granted Dec 22, 1992·21 cites·7 claims
- 1952US5996333AOxidizer control device for a gas turbine engineSNECMA·Filed 1997·Granted Dec 7, 1999·15 cites·3 claims
- 2044US6155055ASeparator for a two-head combustor chamberSNECMA·Filed 1999·Granted Dec 5, 2000·10 cites·18 claims
- 2131US5230212AOxidizer supply control system for a gas turbine engineMOTEURS S N E C M A SOC NAT D·Filed 1992·Granted Jul 27, 1993·6 cites·12 claims
- 2226US4525135AApparatus for molding and perforating a FRP sheetSNECMA·Filed 1984·Granted Jun 25, 1985·2 cites·4 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →